Robust attitude controller design of linear parameter varying spacecraft via μ synthesis and gain scheduling

IEEE Conference on Control Applications - Proceedings

Volumn 2, Issue , 1999, Pages 979-984

  Nagashio, Tomoyoki ^a   Kida, Takashi ^a  

^a UNIVERSITY OF ELECTRO COMMUNICATIONS   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM SYNTHESIS; GAIN CONTROL; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; MOTION CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; VIBRATIONS (MECHANICAL);

ATTITUDE CONTROLLER; FLEXIBLE SOLAR PADDLES; GAIN SCHEDULING; LINEAR PARAMETER VARYING SPACECRAFT;

SPACECRAFT;

EID: 0033356827     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)